DE602008002722D1 - SPOILER FOR AN AERODYNAMIC BODY OF AN AIRCRAFT - Google Patents

SPOILER FOR AN AERODYNAMIC BODY OF AN AIRCRAFT

Info

Publication number
DE602008002722D1
DE602008002722D1 DE602008002722T DE602008002722T DE602008002722D1 DE 602008002722 D1 DE602008002722 D1 DE 602008002722D1 DE 602008002722 T DE602008002722 T DE 602008002722T DE 602008002722 T DE602008002722 T DE 602008002722T DE 602008002722 D1 DE602008002722 D1 DE 602008002722D1
Authority
DE
Germany
Prior art keywords
air flow
spoiler
aircraft
segments
flow direction
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
DE602008002722T
Other languages
German (de)
Inventor
Timo Voss
Joachim Loerke
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of DE602008002722D1 publication Critical patent/DE602008002722D1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C2009/143—Adjustable control surfaces or members, e.g. rudders forming slots comprising independently adjustable elements for closing or opening the slot between the main wing and leading or trailing edge flaps

Abstract

The invention pertains to a spoiler (5) for an aerodynamically active surface of an aircraft (1), particularly for an airfoil of an aircraft, wherein said spoiler is supported on the aerodynamically active surface such that it is articulated about an axis (11) extending transverse to the air flow direction and can be adjusted relative to the air flow. According to the invention, the spoiler features two or more segments (6, 7) that are arranged behind one another referred to the air flow direction and extend transverse to the air flow direction, wherein said segments are connected to one another in an articulated fashion and can be adjusted to different angles referred to the air flow. The successively arranged segments of the spoiler (5) can be actuated, in particular, by means of an actuating device (8, 9, 10) in such a way that the rear segment (7) is adjusted relative to the air flow by a greater angle than the front segment (6).
DE602008002722T 2007-02-23 2008-02-25 SPOILER FOR AN AERODYNAMIC BODY OF AN AIRCRAFT Active DE602008002722D1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007009060A DE102007009060A1 (en) 2007-02-23 2007-02-23 Spoiler for an aerodynamically effective surface of an aircraft
PCT/EP2008/001481 WO2008101735A1 (en) 2007-02-23 2008-02-25 Spoiler for an aerodynamic body of an aircraft

Publications (1)

Publication Number Publication Date
DE602008002722D1 true DE602008002722D1 (en) 2010-11-04

Family

ID=39400074

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102007009060A Withdrawn DE102007009060A1 (en) 2007-02-23 2007-02-23 Spoiler for an aerodynamically effective surface of an aircraft
DE602008002722T Active DE602008002722D1 (en) 2007-02-23 2008-02-25 SPOILER FOR AN AERODYNAMIC BODY OF AN AIRCRAFT

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE102007009060A Withdrawn DE102007009060A1 (en) 2007-02-23 2007-02-23 Spoiler for an aerodynamically effective surface of an aircraft

Country Status (7)

Country Link
US (1) US8651430B2 (en)
EP (1) EP2125510B1 (en)
CN (1) CN101668681B (en)
AT (1) ATE482139T1 (en)
DE (2) DE102007009060A1 (en)
RU (1) RU2452657C2 (en)
WO (1) WO2008101735A1 (en)

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* Cited by examiner, † Cited by third party
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GB0902685D0 (en) * 2009-02-18 2009-04-01 Airbus Uk Ltd Aircraft wing assembly
JP5562575B2 (en) * 2009-04-27 2014-07-30 ナブテスコ株式会社 Aircraft actuator
GB201108450D0 (en) * 2011-05-20 2011-07-06 Airbus Operations Ltd Aircraft wing assembly
WO2013172914A2 (en) * 2012-02-27 2013-11-21 Sinhatech Self adjusting deturbulator enhanced flap and wind deflector
RU2522638C2 (en) * 2012-07-25 2014-07-20 Российская Федерация, От Имени Которой Выступает Министерство Промышленности И Торговли Российской Федерации Electromechanical drive of aircraft wing interceptor
CN102929150B (en) * 2012-11-13 2015-02-11 湖南航天机电设备与特种材料研究所 Spoiler self-adaptive control method based on discrete control model
US9446835B2 (en) * 2013-01-16 2016-09-20 Otto Aviation Group Aircraft wing
GB2512318A (en) * 2013-03-26 2014-10-01 Eads Uk Ltd Lift-reducing apparatus for aircraft wings
CN105083537A (en) * 2015-08-05 2015-11-25 北京韦加航通科技有限责任公司 Control surface control device and aircraft
EP3187412B1 (en) * 2015-12-30 2020-03-11 Airbus Defence and Space GmbH Aircraft wing with an adaptive shock control bump
EP3187413B1 (en) * 2015-12-30 2019-07-03 Airbus Defence and Space GmbH Aircraft wing with spoiler
DE102016210407B4 (en) * 2016-06-13 2022-12-01 Röchling Automotive SE & Co. KG Front spoiler arrangement with a flow guide component that can be decoupled from the movement drive as overload protection
CN107554804B (en) * 2016-07-01 2020-12-29 空中客车简化股份公司 Support device for actuator, air intake system and aircraft
CN108791539A (en) * 2018-06-05 2018-11-13 广东工业大学 A kind of regulating device of macro micro- combination
CN108791817B (en) * 2018-06-26 2021-07-20 深圳市飞翼创新有限公司 Aircraft propeller with low resistance performance and assembling method thereof
US11352123B2 (en) 2018-06-28 2022-06-07 Lucas Kai-Luen Hung Wing assembly for a high endurance aircraft
US11001371B2 (en) * 2018-08-07 2021-05-11 The Boeing Company Hydraulic droop control for aircraft wing
US11072415B2 (en) * 2018-08-24 2021-07-27 Spirit Aerosystems, Inc. Nacelle aerodynamic spoiler
US10926865B2 (en) 2018-12-11 2021-02-23 The Boeing Company Spoiler with releasable portion
US11254417B2 (en) 2018-12-11 2022-02-22 The Boeing Company Multi-section spoiler
US11548616B1 (en) 2020-03-02 2023-01-10 Lucas Kai-Luen Hung Split-flap wing assembly for a high endurance aircraft
CN114572381A (en) * 2022-04-19 2022-06-03 中国商用飞机有限责任公司 Tail cone with speed reducing assembly and airplane provided with tail cone

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US202089A (en) * 1878-04-09 Improvement in pipe-tongs
US2006391A (en) * 1933-05-18 1935-07-02 Zantford D Granville Airplane controls
US2152835A (en) * 1937-03-13 1939-04-04 Bolas Harold Aircraft
US2418273A (en) * 1944-12-26 1947-04-01 Willard H Moore Aircraft wing flap assembly
FR1496152A (en) * 1966-06-20 1967-09-29 Giravions Dorand Airplane wing nozzle or blown helicopter blade
US3756089A (en) * 1971-04-15 1973-09-04 H Haladay Linkage for narrow environments
DE2125971C3 (en) * 1971-05-26 1978-08-03 Vereinigte Flugtechnische Werkefokker Gmbh, 2800 Bremen Flap arrangement for an aircraft wing
US4120470A (en) * 1976-09-28 1978-10-17 The Boeing Company Efficient trailing edge system for an aircraft wing
SU845355A1 (en) * 1980-01-04 2004-08-20 О.А. Артемов DEVICE FOR INCREASING STABILITY OF THE AIRCRAFT
US4932613A (en) * 1988-06-24 1990-06-12 Curtiss-Wright Flight Systems, Inc. Rotary hinge actuator
US5098043A (en) * 1990-02-27 1992-03-24 Grumman Aerospace Corporation Integrated power hinge actuator
FR2728535A1 (en) * 1994-12-26 1996-06-28 Aerospatiale VARIABLE SLOTTED AEROBRAKE FOR AIRCRAFT WING
SE9601956D0 (en) * 1996-05-22 1996-05-22 Saab Ab Segmented flap with variable curvature for aircraft wing
FR2859976B1 (en) * 2003-09-22 2006-12-08 Airbus France AIRCRAFT WING COMPRISING AT LEAST ONE DEPORTER SHUTTER AND DEPORTER SHUTTER FOR SAID WING
DE102004049504A1 (en) 2004-10-11 2006-04-13 Airbus Deutschland Gmbh Wing for aircraft has a rear auxiliary lift flap coupled to main wing and able to lie against main wing in retracted position and form air gap with it when extended
US7338018B2 (en) * 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
DE102007055669A1 (en) * 2007-11-21 2009-06-04 Airbus Deutschland Gmbh Landing flap kinematics powered by pinion drive
ITTO20080566A1 (en) * 2008-07-23 2010-01-24 Alenia Aeronautica Spa ACTUATOR DEVICE BASED ON ALLOY OF SHAPE MEMORY AND FLAP GROUP FLYWHEEL EQUIPPED WITH SUCH AN ACTUATOR DEVICE

Also Published As

Publication number Publication date
DE102007009060A1 (en) 2008-08-28
US20100320332A1 (en) 2010-12-23
RU2452657C2 (en) 2012-06-10
RU2009135274A (en) 2011-03-27
EP2125510B1 (en) 2010-09-22
EP2125510A1 (en) 2009-12-02
CN101668681A (en) 2010-03-10
WO2008101735A1 (en) 2008-08-28
CN101668681B (en) 2013-06-05
ATE482139T1 (en) 2010-10-15
US8651430B2 (en) 2014-02-18

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